Print assembly for additive manufacturing system, and methods of use thereof

ABSTRACT

A print assembly for use in an additive manufacturing system to print three-dimensional parts, which includes a coarse positioner, a fine positioner, and a liquefier assembly, where a portion of the liquefier assembly is operably mounted to the fine positioner such that the fine positioner is configured to move the portion of the liquefier assembly relative to the coarse positioner.

CROSS-REFERENCE TO RELATED APPLICATION(S)

This Application is a continuation of U.S. patent application Ser. No.16/919,395, filed on Jul. 2, 2020, which is a continuation of U.S.patent application Ser. No. 15/514,740 filed on Mar. 27, 2017, entitledPRINT ASSEMBLY FOR ADDITIVE MANUFACTURING SYSTEM, AND METHODS OF USETHEREOF, now U.S. Pat. No. 10,744,753, which issued on Aug. 18, 2020,which is a 371 National Stage Application of International ApplicationNo. PCT/US2015/052681, filed on Sep. 28, 2015, and published asInternational Publication No. WO2016/049640, which claims priority toU.S. Patent Application No. 62/056,200, filed on Sep. 26, 2014 and U.S.Patent Application No. 62/056,186, filed on Sep. 26, 2014, the contentsof which are incorporated by reference in their entireties.

BACKGROUND

The present disclosure relates to additive manufacturing systems forprinting or otherwise producing three-dimensional (3D) parts and supportstructures. In particular, the present disclosure relates to printassemblies having liquefier assemblies and associated roboticpositioners (e.g., gantries) for printing 3D parts and supportstructures in a layer-by-layer manner using an additive manufacturingtechnique.

Additive manufacturing systems are used to print or otherwise build 3Dparts from digital representations of the 3D parts (e.g., AMF and STLformat files) using one or more additive manufacturing techniques.Examples of commercially available additive manufacturing techniquesinclude extrusion-based techniques, jetting, selective laser sintering,powder/binder jetting, electron-beam melting, digital light processing(DLP), and stereolithographic processes. For each of these techniques,the digital representation of the 3D part is initially sliced intomultiple horizontal layers. For each sliced layer, a tool path is thengenerated, which provides instructions for the particular additivemanufacturing system to print the given layer.

For example, in an extrusion-based additive manufacturing system, a 3Dpart may be printed from a digital representation of the 3D part in alayer-by-layer manner by extruding a flowable part material. The partmaterial is extruded through an extrusion tip carried by a print head ofthe system, and is deposited as a sequence of roads on a platen inplanar layers. The extruded part material fuses to previously depositedpart material, and solidifies upon a drop in temperature. The positionof the print head relative to the substrate is then incremented, and theprocess is repeated to form a 3D part resembling the digitalrepresentation.

In fabricating 3D parts by depositing layers of a part material,supporting layers or structures are typically built underneathoverhanging portions or in cavities of 3D parts under construction,which are not supported by the part material itself. A support structuremay be built utilizing the same deposition techniques by which the partmaterial is deposited. The host computer generates additional geometryacting as a support structure for the overhanging or free-space segmentsof the 3D part being formed. Support material is then deposited pursuantto the generated geometry during the printing process. The supportmaterial adheres to the part material during fabrication, and isremovable from the completed 3D part when the printing process iscomplete.

SUMMARY

An aspect of the present disclosure is directed to a print assembly foruse in an additive manufacturing system to print 3D parts. The printassembly includes a coarse positioner, a fine positioner, and aliquefier assembly, where a portion of the liquefier assembly isoperably mounted to the fine positioner such that the fine positioner isconfigured to move the portion of the liquefier assembly relative to thecoarse positioner.

Another aspect of the present disclosure is directed to a print assemblyfor use in an additive manufacturing system to print 3D parts, whichincludes a first robotic positioner, and a second robotic positionerthat is operably mounted to the first robotic positioner such that thefirst robotic positioner is configured to move the second roboticpositioner over a first range of motion. The print assembly alsoincludes a liquefier assembly having a first stage and a second stageconnected to the first stage, where the second stage is mounted to thesecond robotic positioner, and where the second robotic positioner isconfigured to move the second stage of the liquefier assembly in asecond range of motion relative to the first robotic positioner that isless than the first range of motion of the first robotic positioner.

Another aspect of the present disclosure is directed to a print assemblyfor use in an additive manufacturing system to print 3D parts, whichincludes a first robotic positioner, and a second robotic positionerthat is operably mounted to the first robotic positioner such that thefirst robotic positioner is configured to move the second roboticpositioner, where the second robotic positioner has a higher fundamentalresonance frequency than the first robotic positioner, and a liquefierassembly configured to melt and extrude a consumable material, where aportion of the liquefier assembly is operably mounted to the secondrobotic positioner.

Another aspect of the present disclosure is directed to a print assemblyfor use in an additive manufacturing system to print 3D parts, whichincludes a coarse positioner, a fine positioner operably mounted to thecoarse positioner such that the coarse positioner is configured to movethe fine positioner in an x-y plane, and a liquefier assembly comprisinga first stage and a second stage connected to the first stage, where thesecond stage is mounted to the fine positioner, and where the finepositioner is configured to move the second stage of the liquefierassembly relative to the coarse positioner.

Another aspect of the present disclosure is directed to an additivemanufacturing system for printing 3D parts. The additive manufacturingsystem includes a first robotic positioner, a second robotic positioneroperably mounted to the first robotic positioner, and a liquefierassembly comprising a first stage and a second stage, where the secondstage is operably mounted to the second robotic positioner. The systemalso includes a controller assembly configured to command the firstrobotic positioner to move the second robotic positioner, to command thesecond robotic positioner to move the second stage of the liquefierassembly relative to the first robotic positioner, and to command theliquefier assembly to controllably melt and extrude a consumablematerial.

Another aspect of the present disclosure is directed to a method forprinting a 3D part with an additive manufacturing system. The methodincludes moving a fine positioner in an x-y plane with a coarsepositioner, moving (with the fine positioner) a portion of a liquefierassembly in the x-y plane relative to the coarse positioner, and meltingand extruding a consumable material in the liquefier assembly to printthe 3D part in a layer-by-layer manner.

Another aspect of the present disclosure is directed to a print assemblyfor use in an additive manufacturing system to print 3D parts, whichincludes a first robotic positioner, and a second robotic positioneroperably mounted to the first robotic positioner such that the firstrobotic positioner is configured to move the second robotic positionerover a first range of motion. The print assembly also includes aliquefier assembly having a first portion (e.g., a first stage, aliquefier stage, a liquefier portion, and the like) and a second portion(e.g., a second stage, an accumulator stage, an extrusion nozzle, andthe like) connected to the first portion (e.g., with a conduit), whereinthe second portion is mounted to the second robotic positioner, andwherein the second robotic positioner is configured to move the secondportion of the liquefier assembly in a second range of motion relativeto the robotic positioner that is less than the first range of motion ofthe first robotic positioner.

Definitions

Unless otherwise specified, the following terms as used herein have themeanings provided below:

The term “operably connected”, with reference to articles being operablyconnected to each other, refers to direct connections (physically incontact with each other) and indirect connections (connected to eachother with one or more additional components, such as spacers, disposedbetween them).

The terms “command”, “commanding”, and the like, with reference to acontroller assembly commanding a device (e.g., a drive mechanism, anactuator, or the like), refers to the direct and/or indirect relaying ofcontrol signals from the controller assembly to the device such that thedevice operates in conformance with the relayed signals. The signals maybe relayed in any suitable form, such as communication signals to amicroprocessor on the device, applied electrical power to operate thedevice, and the like.

The terms “preferred” and “preferably” refer to embodiments of theinvention that may afford certain benefits, under certain circumstances.However, other embodiments may also be preferred, under the same orother circumstances. Furthermore, the recitation of one or morepreferred embodiments does not imply that other embodiments are notuseful, and is not intended to exclude other embodiments from the scopeof the present disclosure.

Directional orientations such as “above”, “below”, “top”, “bottom”, andthe like are made with reference to a layer-printing direction of a 3Dpart. In the embodiments shown below, the layer-printing direction isthe upward direction along the vertical z-axis. In these embodiments,the terms “above”, “below”, “top”, “bottom”, and the like are based onthe vertical z-axis. However, in embodiments in which the layers of 3Dparts are printed along a different axis, such as along a horizontalx-axis or y-axis, the terms “above”, “below”, “top”, “bottom”, and thelike are relative to the given axis.

The term “providing”, such as for “providing a material”, when recitedin the claims, is not intended to require any particular delivery orreceipt of the provided item. Rather, the term “providing” is merelyused to recite items that will be referred to in subsequent elements ofthe claim(s), for purposes of clarity and ease of readability.

Unless otherwise specified, temperatures referred to herein are based onatmospheric pressure (i.e. one atmosphere).

The terms “at least one” and “one or more of” an element are usedinterchangeably, and have the same meaning that includes a singleelement and a plurality of the elements, and may also be represented bythe suffix “(s)” at the end of the element.

The terms “about” and “substantially” are used herein with respect tomeasurable values and ranges due to expected variations known to thoseskilled in the art (e.g., limitations and variabilities inmeasurements).

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a front view of an additive manufacturing system configured toprint 3D parts and support structures with the use of a print assemblyof the present disclosure.

FIG. 2A is a top view of the print assembly.

FIG. 2B is a top view of an alternative embodiment for the printassembly, in which liquefier assemblies and fine positioners are securedto individual effectors of a coarse positioner.

FIG. 2C is a top view of another alternative embodiment for the printassembly, in which in which each liquefier assembly and fine positioneris used with an individual coarse positioner. This embodiment alsoillustrates a print assembly having a single liquefier assembly and finepositioner.

FIG. 2D is a top view another alternative embodiment for the printassembly, in which the coarse positioner moves a platen, and is separatefrom the fine positioner.

FIG. 3 is a front view of a liquefier stage and a conduit of theliquefier assembly in use with a consumable filament.

FIG. 4 is a inlet end view of the liquefier stage.

FIG. 5 is a top perspective view of an accumulator stage and conduit ofthe liquefier assembly in use with the fine positioner.

FIG. 6 is a top perspective view of the accumulator stage.

FIG. 7 is a front view of an accumulator of the accumulator stageintegrally formed with the conduit, and secured to a nozzle.

FIG. 8 is an inlet end view of the accumulator stage.

FIG. 9 is a schematic illustration of a controller assembly of theadditive manufacturing system in use with the print assembly.

FIG. 10 is a graphical illustration of a tool path segment having sharp,180-degree turn.

FIG. 11 is a graphical illustration of y-axis positions for the coarsepositioner and the fine positioner while traversing the tool pathsegment shown in FIG. 10.

FIG. 12 is a graphical illustration of extrudate volumetric flow rateswhile traversing the tool path segment shown in FIG. 10.

FIG. 13 is a perspective view of an alternative liquefier assembly, inwhich the upstream liquefier stage includes a cylindrical liquefier.

FIG. 14 is a perspective view of another alternative liquefier assembly,in which the upstream liquefier stage includes a screw pump.

FIG. 15 is a perspective view of another alternative liquefier assembly,in which multiple upstream liquefier stages are used with a commondownstream accumulator stage.

FIG. 16 is an infrared photograph of an example self-heating conduittest.

DETAILED DESCRIPTION

The present disclosure is directed to a print assembly for use in anadditive manufacturing system to print 3D parts and support structuresin a layer-by-layer manner using an additive manufacturing technique.The print assembly includes two or more robotic positioners (e.g.,gantries) that provide a coarse-fine position control. The printassembly also includes one or more liquefier assemblies retained by therobotic positioners for melting and extruding consumable materials toprint the 3D parts and support structures. Preferably, the liquefierassemblies are multiple-stage liquefier assemblies, althoughsingle-stage liquefier assemblies may also optionally be used.

As discussed below, the print assembly overcomes multiple limitations incurrent print head gantries, such as acceleration and decelerationlimitations due to fundamental or natural resonance frequencies of theprint head gantries. In particular, the print assembly can effectivelyprovide a coarse-fine position control (with the robotic positioners),as well as a coarse-fine extrusion control (with the multiple-stageliquefier assemblies). This allows the print assembly to produce 3Dparts with good part resolutions and fast printing speeds, evennegotiating when tortuous tool paths, such as tool paths with sinusoidalgeometries, sharp corners, sharp 180-degree turns, and the like.

The print assembly may be used with any suitable additive manufacturingsystem. For instance, system 10 is an example additive manufacturingsystem for printing 3D parts or models and corresponding supportstructures (e.g., 3D part 12 and support structure 14) using alayer-based, additive manufacturing technique. Suitable additivemanufacturing systems for system 10 include extrusion-based systemsdeveloped by Stratasys, Inc., Eden Prairie, Minn., such as fuseddeposition modeling systems under the trademark “FDM”. In the shownembodiment, 3D part 12 and support structure 14 are respectively printedfrom part and support materials of consumable assemblies 16 with the useof print assembly 18 of the present disclosure, where print assembly 18includes a pair of liquefier assemblies 20 (only a single liquefierassembly 20 is shown in FIG. 1, the second being located behind it).

Consumable assemblies 16 each include a container portion 22, which isan easily loadable, removable, and replaceable container device thatretains a supply of a consumable filament for printing with system 10.Each container portion 22 may retain the consumable filament on a woundspool, a spool-less coil, or other supply arrangement, such as discussedin Swanson et al., U.S. Pat. No. 7,374,712; Taatjes at al., U.S. Pat.No. 7,938,356; Mannella et al., U.S. Publication Nos. 2013/0161432 and2013/0161442; and Batchelder et al., U.S. Publication No. 2014/0158802.

In alternative embodiments, container portions 22 may be replaced withother supply sources of consumable materials, where the consumablematerials may be any suitable media type, such as filaments, powders,pellets, slugs, and the like. For instance, in embodiments in which theconsumable materials are provided in powder form, container portions 22may be replaced with one or more hoppers, such as discussed in Bosveldet al., U.S. Publication No. 2013/0333798.

Each container portion 22 preferably engages with a guide tube 24, whichinterconnects the container portion 22 to its associated print assembly18. Accordingly, drive mechanisms of print assembly 18 (and/or of system10) draw successive segments of the consumable filaments from containerportions 22, through guide tubes 24, to the liquefier assemblies 20 ofprint assembly 18.

In some embodiments, print assembly 18 and guide tubes 24 are fixedsub-components of system 10, and each consumable assembly 16 includes acontainer portion 22 and the retained consumable filament. However, inalternative embodiments, portions of print assembly 18, containerportion 22, and guide tube 24 are sub-components of consumable assembly16, such that the given portions of print assembly 18, container portion22, and guide tube 24 are collectively replaced in an interchangeablemanner, as discussed in Swanson, U.S. Pat. No. 8,403,658.

As further shown in FIG. 1, system 10 includes also system casing 26,chamber 28, platen 30, and platen gantry 32. System casing 26 is astructural component of system 10 and may include multiple structuralsub-components such as support frames, housing walls, and the like. Insome embodiments, system casing 26 may include container bays or otherreceiving areas configured to receive container portions 22 ofconsumable assemblies 16. In alternative embodiments, the container baysmay be omitted to reduce the overall footprint of system 10. In theseembodiments, container portions 22 may stand adjacent to system casing26, while providing sufficient ranges of movement for guide tubes 24 andliquefier assemblies 20.

Chamber 28 is an example build environment that contains platen 30 forprinting 3D part 12 and support structure 14, where chamber 28 may bemay be optionally omitted and/or replaced with different types of buildenvironments. For example, 3D part 12 and support structure 14 may bebuilt in a build environment that is open to ambient conditions or maybe enclosed with alternative structures (e.g., flexible curtains). Inthe shown example, the interior volume of chamber 28 may be heated withheater 28 h to reduce the rate at which the part and support materialssolidify after being extruded and deposited (e.g., to reduce distortionsand curling). Heater 28 h may be any suitable device or assembly forheating the interior volume of chamber 28, such as by radiant heatingand/or by circulating heated air or other gas (e.g., inert gases). Inalternative embodiments, heater 28 h may be replaced with otherconditioning devices, such as a cooling unit to generate and circulatecooling air or other gas. The particular thermal conditions for thebuild environment may vary depending on the particular consumablematerials used.

Platen 30 is a platform on which 3D part 12 and support structure 14 areprinted in a layer-by-layer manner, and is supported by platen gantry32. In some embodiments, platen 30 may engage and support a buildsubstrate, which may be a tray substrate as disclosed in Dunn et al.,U.S. Pat. No. 7,127,309; may be fabricated from plastic, corrugatedcardboard, or other suitable material; and may also include a flexiblepolymeric film or liner, painter's tape, polyimide tape, adhesivelaminate (e.g., an applied glue), or other disposable fabrication foradhering deposited material onto the platen 30 or onto the buildsubstrate. In some embodiments, platen 30 and/or the build substrate maybe heated, such as with one or more electrically-resistive heatingelements.

Platen gantry 32 is a robotic positioner (e.g., a gantry) configured tomove platen 30 along (or substantially along) the vertical z-axis.Platen gantry 32 may operate with one or more motors (e.g., steppermotors and encoded DC motors), gears, pulleys, belts, screw drives,linear portals, robotic arms, delta configurations, hexapods, and thelike. As discussed below, in some embodiments, platen gantry 32 mayfunction as a coarse positioner of print assembly 18. In otherembodiments, platen gantry 32 may be omitted, and platen 30 may befixedly mounted in chamber 28.

System 10 also includes controller assembly 34, which is one or morecomputer-based systems configured to operate the components of system10. Controller assembly 34 may communicate over communication line 36with the various components of system 10, such as print assembly 18,chamber 28 (e.g., heater 28 h), head carriage 34, motors for platengantry 32, and various sensors, calibration devices, display devices,and/or user input devices. In some embodiments, controller assembly 34may also communicate with one or more of platen 30, platen gantry 32,and any other suitable component of system 10.

Additionally, controller assembly 34 may also communicate overcommunication line 38 with external devices, such as other computers andservers over a network connection (e.g., an internet connection, a localarea network (LAN) connection, a universal serial bus (USB) connection,a cellular connection, and the like). While communication lines 36 and38 are each illustrated as a single signal line, they may each includeone or more electrical, optical, and/or wireless signal lines andintermediate control circuits, where portions of communication line(s)36 may also be subcomponents of print assembly 18. For instance, in someembodiments, communication line(s) 36 may include wireless componentsfor communicating with devices that accelerate and decelerate quickly(e.g., high-g-force gantries), where physical cable reliability couldpotentially be an issue.

In some embodiments, the one or more computer-based systems ofcontroller assembly 34 are internal to system 10, allowing a user tooperate system 10 over a network communication line 38, such as from anexternal computer in the same or similar manner as a two-dimensionalprinter. Alternatively, controller assembly 34 may also include one ormore external computer-based systems (e.g., desktop, laptop,server-based, cloud-based, tablet, mobile media device, and the like)that may communicate with the internal computer-based system(s) ofcontroller assembly 34, as well as communicating over a network viacommunication line 38.

In this alternative embodiment, the processing functions of controllerassembly 34 discussed below may be divided between the internal andexternal computer-based systems. In yet another alternative embodiment,the computer-based system(s) of controller assembly 34 may all belocated external to system 10 (e.g., one or more external computers),and may communicate with system 10 over communication line 36.

Current extrusion-based additive manufacturing or 3D printing systemshave gained popularity in a variety of industries due to theircapabilities for printing strong 3D parts from a variety of materials,with low support material requirements, accurate depositions, andrelatively low costs. However, there has been an increasing demand forhigher-resolution parts and faster printing speeds, which can push thelimits of what current extrusion-based systems can achieve in terms ofaccuracies and printing speeds.

For example, current head gantries are capable of moving print headsalong linear and other simple tool paths at high velocities withaccurate depositions. However, the print heads are typically slowed downto negotiate tortuous tool paths, such as tool paths with sinusoidalgeometries, sharp corners, sharp 180-degree turns, and the like. Inthese cases, the print heads also typically reduce their extrudatevolumetric flow rates when negotiating the corners to maintain accuratedeposition volumes.

As such, to preserve printing speeds as much as possible, it isdesirable to have a print head travel into a tortuous tool path (e.g., asharp corner) at a fast velocity, decelerate quickly and negotiate thetortuous tool path, and then quickly accelerate back up to the fastvelocity. This minimizes the time that the print head remains at thereduced velocity, which can otherwise accumulate over numerous tortuoustool paths in a 3D part.

The accelerations and decelerations of a print head, however, arelimited by the fundamental or natural resonance frequency of the gantrymoving the print head. If a gantry accelerates or decelerates the printhead too quickly, for example, such that the natural gantry resonancesare excited, it will induce x-y position errors that can reducedeposition accuracies. As such, there is a physical limit to how fast aprint head can be accelerated and decelerated (to increase overallprinting speeds) without detrimentally affecting the depositionaccuracies.

The print assembly 18, however, is capable of increasing printing speedsbeyond the physical limits of current single-stage gantries, while alsopreserving deposition accuracies. This is achieved through the use oftwo or more robotic positioners having increasing-positional accuraciesin the x-y plane. For example, as shown in FIG. 2A, print assembly 18may include a shared coarse positioner 40, as well as a pair offine-position gantries 42. As mentioned above, print assembly 18 alsoincludes a pair of liquefier assemblies 20, each of which is preferablya multiple-stage assembly. For instance, each liquefier assembly 20 mayinclude an upstream liquefier stage 44, an interconnecting conduit 46,and a downstream accumulator stage 48. Alternatively, in embodiments inwhich liquefier assembly 20 is a single-stage liquefier assembly,downstream accumulator stage 48 may be replaced with an extrusionnozzle, where the drive control is determined by liquefier stage 44.

Coarse positioner 40 is a first robotic positioner that includes one ormore motors 50, gantry rails 52, and effector 54. Motor(s) 50 may be anysuitable motors, such as one or more stepper motors, encoded DC motors,hydraulic motors, piezoelectric motors, and the like. Based on commandsfrom controller assembly 38, motor(s) 50 operably move effector 54 alonggantry rails 52 in (or substantially in) a horizontal x-y plane aboveplaten 30, or at least along a single axis.

Examples of suitable robotic positioners for coarse positioner 40include those disclosed in Swanson et al., U.S. Pat. No. 6,722,872; andComb et al., U.S. Publication No. 2013/0078073, where coarse positioner40 may also support deformable baffles (not shown) that define a ceilingfor chamber 28. While illustrated as a bridge-type gantry, coarsepositioner 40 may utilize any suitable robotic mechanism for movingeffector 54, such as with gears, pulleys, belts, screw drives, linearportals, robotic arms, delta configurations, hexapods, and the like.

As shown, coarse positioner 40 moves effector 54 in the x-y plane aboveplaten 30, where effector 54 itself retains liquefier assemblies 20 andfine positioner 42. This can result in a payload up to about 5 or even10 pounds. Due to its larger size and payload requirements, coarsepositioner 40 has a lower fundamental resonance frequency, whichrestricts its ability to quickly accelerate and decelerate effector 54.For example, coarse positioner 40 may accelerate and decelerate effector54 with up to about ten gees, more typically up to about five gees, andin some cases, up to about three gees, without inducing x-y positionerrors. While coarse positioner 40 may alternatively be manufactured tohave a higher fundamental resonance frequency (e.g., using stiffermaterials), such gantries can be very expensive to produce, renderingthem less suitable for lower-cost designs.

Effector 54 is a first carriage or other effector unit movably supportedby gantry rails 52, and, in the shown embodiment, is shared by the pairof liquefier assemblies 20 and fine positioners 42. Accordingly,effector 54 may securely retain and support each fine positioner 42 andeach upstream liquefier stage 44, preferably in a manner that preventsor restricts their movements relative to effector 54. Effector 54 alsopreferably includes one or more encoders, tachometers, accelerometers,and/or other motion-control sensors 55 located adjacent to one or bothof fine positioners 42, where sensor(s) 55 may communicate withcontroller assembly over communication line 36.

Each fine positioner 42 is a second robotic positioner that includesminiactuator 56 and effector 58. Based on commands from controllerassembly 34, miniactuator 56 may move effector 58 in the x-y plane aboveplaten 30 in a manner that supplements the movements of effector 54 (bycoarse positioner 40). In some embodiments, miniactuator 56 may alsomove effector 58 along the z-axis, such as for servoing or toggling oneor both effectors 58 and accumulator stages 48 between active andstandby states for selective deposition of the consumable materials.

In comparison to coarse positioner 40, each fine positioner 42 has ahigh fundamental resonance frequency, allowing it to quickly accelerateand decelerate its associated effector 58. For example, fine positioner42 can accelerate and decelerate effector 58 (and the retainedaccumulator stage 48) with maximum rates greater than about 30 gees,more preferably greater than about 40 gees, and in some embodiments onthe order of about 50 gees or greater, without inducing x-y positionerrors.

However, due its smaller size, fine positioner 42 is limited to a smallrange of motion in the x-y plane, such up to about one square inch. Assuch, the fast accelerations and decelerations of fine positioner 42 maysupplement the slower accelerations and decelerations of coarsepositioner 40 to achieve accurate depositions at fast printing speeds,even when negotiating tortuous tool paths.

Each effector 58 is a second effector unit movably supported by itsassociated miniactuator 56. Each effector 58 may securely retain andsupport its associated accumulator stage 48 in a manner that prevents orrestricts its movement relative to effector 58.

As further shown in FIG. 2A, coarse positioner 40 may also retain one ormore torque compensators, such as torque compensator 59. Torquecompensator(s) 59 is a motor configured to counteract or otherwisedampen the high-speed torques generated by fine positioners 42.

As mentioned above, each liquefier assembly 20 is separated intomultiple stages, such as upstream liquefier stage 44 and downstreamaccumulator stage 48 (connected by conduit 46). The multiple stages arepreferred because, in order to achieve the fast accelerations anddecelerations, fine positioner 42 cannot carry heavy loads. In fact, thelow-mass payload limit of fine positioner 42 can be less than about 50grams, less than about 20 grams, or even less than about 10 grams. Thispayload limit is significantly less than the weights of currentextrusion-based print heads. Accordingly, separating liquefier assembly20 into multiple stages allows the heavier components (e.g., liquefierstage 44) to be securely mounted on effector 54 of coarse positioner 40(or at a fixed location in system 10), and allows the lighternozzle-portion (e.g., accumulator stage 48) to be mounted on effector 58of fine positioner 42.

Of course, this solution can create an issue with response time delays.Briefly, there is a time response delay between when the upstreamliquefier stage 44 is commanded to change the feed rate, and when theextrudate flow rate from the downstream accumulator stage 48 actuallychanges. Accumulator stage 48 may include an actuator mechanism togenerate fast-responding surges and draw backs of the extrudate. Thesefast-responding surges and draw backs can supplement the slower-reactingpumping from the upstream liquefier stage.

While illustrated with two liquefier assemblies 20 and two finepositioners 42, print assembly 18 may alternatively include three ormore liquefier assemblies 20 and three or more fine positioners 42 forprinting three or more consumable materials. Examples of suitablenumbers of liquefier assemblies 20 (and fine positioners 42) for printassembly 18 range from one to ten, from one to eight, from one to six,from one to four, and/or from one to two.

Furthermore, one or more of the fine positioners 42 may be mounted tocoarse positioner 40 with z-axis servo mechanisms (not shown), such aswith magnetic voice-coil mechanisms. In these embodiments, controllerassembly 34 may command the z-axis servo mechanism(s) to servo or togglethe fine positioner(s) 42 between active and standby states forselective deposition of the consumable materials. For example, one ofthe fine positioners 42 may be cammed or otherwise moveable along thez-axis relative to coarse positioner 40, and the other fine positioner42 may be fixedly mounted to coarse positioner 40.

In yet another embodiment, fine positioners 42 are each mounted suchthat the nozzle tips of accumulator stages 48 are substantially levelwith each other along the z-axis. Moreover, in some embodiments,multiple liquefier assemblies 20 may extrude at the same time, where thefine positioners 42 may independently move their respective accumulatorstages 48 in the x-y plane during the simultaneous extrusions. This canfurther increase printing speeds by printing multiple portions of thesame 3D part 12 (or multiple 3D parts 12) at the same time. As can beappreciated, the use of the multiple and separate fine positioners 42and accumulator stages 48 in this manner can provide an additional levelof print control that is not otherwise achievable with print heads thatare fixed relative to each other in the x-y plane.

Additionally, while coarse positioner 40 and effector 54 are eachillustrated as being shared by the multiple liquefier assemblies 20 andfine-position gantries 42, in alternative embodiments, such as shown inFIG. 2B, each liquefier assembly 20 and fine positioner 42 may besecured to and supported by its own effector 54. In this example, eacheffector 54 may share the remaining components of coarse positioner 40(e.g., shared motor(s) 50 and gantry rails 52), where the firsteffectors 54 may be moved together or independently of each other, asdesired.

In further alternative embodiments, such as shown in FIG. 2C, eachliquefier assembly 20 and fine positioner 42 may use its own coarsepositioner 40 (e.g., its own motor(s) 50, gantry rails 52, and effector54). This arrangement is similar to an embodiment in which system 10only operates with a single liquefier assembly 20, such as for printing3D part 12 without a support structure. One benefit of this embodimentis that the payload of each coarse positioner 40 is reduced.

In another alternative arrangement, such as shown in FIG. 2D, platengantry 32 may function as the coarse positioner for moving platen 30(and 3D part 12 and support structure 14) in the horizontal x-y planebelow each accumulator stage 48. In this embodiment, coarse positioner40 may be omitted, and each fine positioner 42 may be mounted at a fixedlocations in or above chamber 28, such that its associated accumulatorstage 48 is positionable over platen 30. Each liquefier stage 44 may bemounted at any suitable fixed location of system 10 (inside or outsideof chamber 28) such that the associated conduit 46 may interconnectstages 44 and 48. A torque compensator 59 (not shown) may alsooptionally be included to counteract or otherwise dampen the high-speedtorques generated by fine positioner 42.

In this case, platen gantry 32 is capable of moving below eachaccumulator stage 48, but is limited to slower accelerations anddecelerations due to its lower fundamental resonance frequency, asdiscussed above for coarse positioner 40. In comparison, each finepositioner 42 is capable of moving its associated effector 58 andaccumulator stage 48 over a small area (e.g., one square inch), but iscapable of achieving fast accelerations and decelerations. As such,controller assembly 34 may command fine positioner 42 to supplement theslower accelerations and decelerations of platen gantry 32 to achieveaccurate depositions at high printing speeds, even when negotiatingtortuous tool paths.

As can be seen from the above embodiments, fine positioner 42 may beoperably secured to and moved by coarse positioner 42 (e.g., as shown inFIGS. 2A-2C), or may be separate from the coarse positioner (e.g., asshown in FIG. 2D). Moreover, as mentioned above, print assembly 18 mayalso incorporate three or more robotic positioners havingincreasing-positional accuracies in the x-y plane. For instance, platengantry 32 may function as a third robotic positioner that operates withcoarse positioner 40 and fine positioner 42. For example, platen gantry32 may be commanded to operate with slower accelerations anddecelerations than coarse positioner 40. In this case, controllerassembly 34 may command coarse positioner 40 to supplement therelatively slower accelerations and decelerations of platen gantry 32,and may also command fine positioner 42 to supplement the relativelyslower accelerations and decelerations of coarse positioner 40.

Other similar arrangements may also be used such that one or both ofplaten 30 and accumulator stage 48 of liquefier assembly 20 are moveablerelative to each other. For instance, coarse positioner 40 may be arobotic arm, delta configuration, hexapod, or other robotic mechanismcapable of moving in all three x-y-z dimensions. In this embodiment,platen gantry 32 may optionally be omitted, platen 30 may be fixedlyretained in chamber 28.

Platen 30 and accumulator stages 48 may also be oriented along differentaxes. For example, platen 30 may be oriented vertically and accumulatorstages 48 may print 3D part 12 and support structure 14 along the x-axisor the y-axis. In another example, platen 30 and/or accumulator stages48 may be moved relative to each other in a non-Cartesian coordinatesystem, such as in a polar coordinate system.

Each liquefier assembly 20 is preferably associated with one or moreconsumable assemblies 16 and guide tubes 24 to feed a consumablefilament (referred to as filament 60) to upstream liquefier stage 44 ofliquefier assembly 20. During a printing operation, controller assembly34 may command platen gantry 32 to move platen 30 to a predeterminedheight within chamber 28. Controller assembly 34 may then command coarsepositioner 40 and/or fine positioner 42 to move accumulator stage 48around in the horizontal x-y plane above platen 30. Controller assembly34 may also command liquefier stages 44 to selectively draw successivesegments of filaments 60 (or other consumable materials) from containerportions 22 and through guide tubes 24, respectively.

The successive segments of each filament 60 are then melted in liquefierstage 44 of the respective liquefier assembly 20 to produce a moltenmaterial. The movement of the solid portion of filament 60 functions asa viscosity pump to push the molten material under pressure fromliquefier stage 44, through conduit 46, and into accumulator stage 48for extrusion.

Upon exiting accumulator stage 48, the resulting extrudate may bedeposited onto platen 30 as a series of roads for printing 3D part 12 orsupport structure 14 in a layer-by-layer manner. For example, 3D part 12or support structure 14 may be printed or otherwise built in threedimensions by producing successive layers of the deposited roads intwo-dimensional, cross-sectional patterns stacked on top of each other.In some applications, such as discussed in Crump, U.S. Pat. No.5,121,329, the deposited roads may also extend into free space above thex-y build plane, such as with vertically-extending curved arcs. Afterthe print operation is complete, the resulting 3D part 12 and supportstructure 14 may be removed from chamber 28, and support structure 14may be removed from 3D part 12. 3D part 12 may then undergo one or moreadditional post-processing steps, as desired.

The following discussion of print assembly 18 is made with reference toa single liquefier assembly 20 and fine positioner 42 in use with acoarse positioner 40 (e.g., as shown in FIG. 2C) with the understandingthat the same discussion may apply to each of the above-discussedembodiments. As shown, liquefier stage 44 includes drive mechanism 62and liquefier portion 64, and may also optionally include a housing (notshown) having any suitable design for protecting drive mechanism 62. Ifa housing is used, guide tube 24 preferably engages the housing orotherwise directs filament 60 into the housing, and liquefier portion 64may extend from the housing. Liquefier stage 44 also preferably includesone or more temperature sensors, pressure sensors, flow sensors, and thelike, which communicate with controller assembly 34 (e.g., viacommunication line 36). As discussed herein liquefier assembly 20 isutilized with fine positioner 42 in use with coarse positioner 40.However, the liquefier assembly 20 can be utilized in any additivemanufacturing system and is not limited to use with fine positioner 42in use with coarse positioner 40.

Drive mechanism 62 is a motorized device for feeding filament 60 (orother consumable material), such as with one or more rotatable wheels,gears, shafts, and/or screws that are operably connected to one or moremotors (e.g., electric stepper and encoded DC motors). Examples ofsuitable devices for drive mechanism 62 include knurled, geared, ortoothed-based wheels, such as discussed in LaBossiere et al., U.S. Pat.Nos. 7,384,255 and 7,604,470. Additional examples includeinternally-threaded components (e.g., helical coils), such as disclosedin Batchelder et al., U.S. Pat. No. 7,896,209; and rotatable,toothed-shafts, such as disclosed in Swanson et al., U.S. Pat. No.8,647,102; and Koop et al., U.S. Publication No. 2014/0159273. In somepreferred embodiments, drive mechanism 62 includes a toothed drive wheelor gear for engagement with a filament 60 having surface tracks alongits length, as discussed in Batchelder et al., U.S. Pat. No. 8,236,227.This allows drive mechanism 62 to feed the tracked filament 60 intoliquefier 68 with a tractor-drive arrangement.

In the shown embodiment, drive mechanism 62 is a filament drivemechanism that is located upstream from liquefier portion 64, and isconfigured to feed successive segments of filament 60 from guide tube 24to liquefier portion 64 under motorized power, based on commands fromcontroller assembly 34. Drive mechanism 62 may also include any suitablebearing surface (e.g., a rotating bearing surface, not shown) configuredto support the opposing side of filament 60 while drive mechanism 62 isengaged with filament 60. As used herein, the terms “upstream” and“downstream” are made with reference to a filament feed direction and amolten material flow direction, as illustrated by arrows 66.

While drive mechanism 62 is illustrated as being positioned directlyupstream from liquefier portion 64, in alternative embodiments, one ormore drive mechanisms may be positioned at any suitable location(s)along the pathway of filament 60 between (and including) container 22and liquefier portion 64. For instance, in some embodiments, a spooldrive mechanism (not shown) may be used to engage with a spool incontainer 22, where the spool holds a wound supply of filament 60. Inthis case, the spool drive mechanism may rotate the spool to feedfilament 60 through guide tube 24 and into liquefier portion 64 (ratherthan directly engaging filament 60).

Alternatively, drive mechanism 62 may engage filament 60 through a portin liquefier portion 64, such as discussed in Batchelder et al., U.S.Pat. No. 7,897,074. In yet another embodiment, drive mechanism 62 may belocated along guide tube 24 between container 22 and liquefier portion64, and engage filament 60 through a port or intersection in guide tube24. Furthermore, multiple drive mechanisms may be used together. Forexample, a first drive mechanism may be used to feed filament 60 fromcontainer 22 to liquefier portion 64. A second drive mechanism (e.g.,drive mechanism 62) retained by effector 54 may then receive the fedfilament 60 from the first drive mechanism, and feed the receivedfilament 60 into liquefier portion 64.

As best shown in FIGS. 3 and 4, liquefier portion 64 may includeliquefier 68, heater assemblies 70, spacers 72 and 74, and frame 76.Liquefier portion 64 is discussed herein as having a ribbon liquefierarchitecture for use with a ribbon filament. The term “ribbon filament”as used herein refers to a filament (e.g., filament 60) having asubstantially rectangular, arcuate, and/or an elliptical cross-sectionalong its longitudinal length, which may include one or more surfacetracks for engaging with drive mechanism 62, such as disclosed inBatchelder et al., U.S. Pat. No. 8,236,227. Correspondingly, the term“ribbon liquefier” as used herein refers to a hollow liquefier (e.g.,liquefier 68) having a substantially rectangular, arcuate, and/or anelliptical hollow, inner-channel cross-section along its longitudinallength.

For each of the ribbon filament and the ribbon liquefier, thecross-section has a width and a thickness, where a maximum extent of thewidth is at least about 2.5 times greater than a maximum extent of thethickness. For a ribbon filament or ribbon liquefier having asubstantially rectangular or arcuate cross-section, the cross-sectionmay have sharp corners (i.e., 90-degree corners) and/or rounded corners.In aspects in which the ribbon filament has an elliptical cross-section,the elliptical cross-section preferably has an eccentricity of about 0.8or greater, and more preferably of about 0.9 or greater. Examples ofsuitable ribbon filaments and ribbon liquefier architectures forfilament 60 and liquefier portion 64 include those discussed inBatchelder et al., U.S. Pat. Nos. 8,221,669; 8,236,227; and 8,439,665.

Liquefier 68 includes opposing faces 68 a and opposing lateral ends 68b, where faces 68 a are the larger dimensions of liquefier 68(corresponding to the width of liquefier 68) and lateral ends 68 b arethe smaller dimensions of liquefier 68 (corresponding to the thicknessof liquefier 68). Liquefier 68 is preferably fabricated from one or morerigid, thermally-conductive materials, such as stainless steel, and maybe fabricated in a variety of different manners. In a first example, thecross-sectional dimensions of liquefier 68 may be attained by flatteningor otherwise collapsing or crushing a cylindrical liquefier, such asaround a shim insert.

Alternatively, liquefier 68 may be produced by stamping a pair of metalsheets into half-sections, which may then be welded or otherwise sealedtogether to attain the desired cross-sectional dimensions. In a furtherexample, a U-shaped trench may be laser cut or otherwise machined into ametal block to form the side walls of liquefier 68, which may then becovered with one or more metal membranes that encase the trench to formthe inner channel In yet another example, liquefier 52 can be formedwith silicon membranes that span a lithographically-formed channel ortrench.

Liquefier 68 also has an inlet end 78 and an outlet end 80, which arepreferably offset from each other along longitudinal axis 82. Inlet end78 is configured to receive filament 60 from drive mechanism 62, whereinlet end 78 and filament 60 preferably have complementarycross-sectional geometries, such as discussed in Batchelder et al., U.S.Pat. Nos. 8,221,669 and 8,439,665. Outlet end 80 is the downstreamportion of liquefier 68 and terminates at conduit 46, preferably with asealed engagement.

Suitable dimensions for liquefier 68 include those discussed inBatchelder et al., U.S. Pat. Nos. 8,221,669 and 8,439,665. In somepreferred embodiments, liquefier 68 has a length along longitudinal axis82 ranging from about 7.6 millimeters (about 0.3 inches) to about 130millimeters (about 5 inches), more preferably from about 50 millimeters(about 2 inches) to about 100 millimeters (about 4 inches). Suitablehollow, inner-channel thicknesses between faces 68 a range from about0.25 millimeters (about 10 mils) to about 2.5 millimeters (about 100mils), and in some embodiments from about 0.76 millimeters (about 30mils) to about 1.3 millimeters (about 50 mils).

Suitable hollow, inner-channel widths between lateral ends 68 b(perpendicular to the inner-channel widths) range from about 2.5millimeters (about 100 mils) to about 10.2 millimeters (about 400 mils),in some embodiments from about 5.1 millimeters (about 200 mils) to about7.6 millimeters (about 300 mils). Suitable wall thicknesses forliquefier 68 range from about 130 micrometers (about 5 mils) to about500 micrometers (about 20 mils). The above-discussed widths andthicknesses for liquefier 68 are based on the maximum extents of thewidths and thicknesses.

Heater assemblies 70 are one or more heating elements configured toconduct heat to liquefier 68 for melting the received filament 60 withinliquefier 68, based on commands (e.g., received electrical power overline 36) from controller assembly 34. For instance, heater assemblies 70may include one or more coils of resistive wire wrapped around liquefier68, one or more heater blocks secured to liquefier 68, one or moreelectrical-resistance heaters secured to liquefier 68, one or moreinductive heating elements, or any other suitable thermoelectric heatingelement(s) for heating liquefier 68 (and optionally, for coolingliquefier 68).

In the shown example, heater assemblies 70 are in mating contact withfaces 68 a of liquefier 68, such as disclosed in Batchelder et al., U.S.Pat. Nos. 8,221,669; 8,236,227; and 8,439,665; and in Batchelder et al.,U.S. patent application Ser. No. 14/046,301. Alternatively (oradditionally), one or more heater assemblies 70 may be located at one orboth lateral ends 68 b of liquefier 68.

Spacers 72 and 74 are each a pair of opposing optional spacer blocks orassemblies disposed between heater assemblies 70 and frame 76. Eachspacer 72 and 74 is preferably produced from one or more materials thatare relatively compliant to provide good mating interfaces betweenliquefier 68, heater assemblies 70, and frame 76, and that are strongenough to resist any expansion or ballooning effects of liquefier 68 dueto internally-generated pressures.

In some embodiments, such as discussed in Batchelder et al., U.S. PatentApplication Publication No. 2015/0097053, the material(s) for one orboth of spacers 72 and 74 may also have modest thermal conductivities todraw heat from liquefier 68 and heater assemblies 70, and may also havesets of indentations (not shown) for thermally isolating separateheating zones. Suitable materials for spacers 72 and 74 include sheetsilicate materials (e.g., sheet mica), aluminum, ceramic materials, andthe like. In some alternative embodiments, spacers 72 and/or spacers 74may be omitted, and liquefier 68 and (optionally) heater assemblies 70may be directly retained by frame 76.

In a further embodiment, liquefier 68 may also incorporate a separatelyunique and beneficial feature. In this embodiment, liquefier 68, whichis preferably thermally and electrically conductive, may directlyreceive an applied electrical current (e.g., via line 36) that cangenerate resistive heating along liquefier 68. Controller assembly 34may also measure and monitor the temperature of liquefier 68 in realtime from the resistance to the applied electrical current (e.g., vialine 36). This effectively provides a self-heating and self-sensingliquefier.

In the shown example, frame 76 is a hollow cylindrical rigid frame forsecurely retaining liquefier 68, heater assemblies 70, and spacers 72and 74, and for mounting liquefier portion 64 to effector 54 (or toanother fixed location in system 10). In alternative embodiments, frame76 may have any suitable geometry, such as a U-shaped, C-shaped, orV-shaped rigid frame, such that frame 76 preferably resists anyexpansion or ballooning effects of liquefier 68 due tointernally-generated pressures. Frame 76 may be fabricated from one ormore materials that provide a strong and rigid structure, such as one ormore metals (e.g., stainless steel and aluminum). In further alternativeembodiments, frame 76 may be omitted, if desired.

During the printing operation, drive mechanism 62 feeds successivesegments of filament 60 into inlet end 78 of liquefier 68. In this case,filament 60 is pushed into inlet end 78. Alternatively, in a portedliquefier embodiment, such as discussed in Batchelder et al., U.S. Pat.No. 7,897,074, where drive mechanism 62 is located downstream from inletend 78, drive mechanism 62 may feed successive segments of filament 60into inlet end 78 by pulling filament 60 into inlet end 78.

As filament 60 passes through liquefier 68 in the direction of arrow 66,heater assemblies 70 thermally melt the received successive segments,where the molten portion of the filament material forms a meniscusaround the unmelted portion of filament 60. The downward or forwardmovement of filament 60 functions as a viscosity pump to push the moltenmaterial through conduit 46 and into accumulator stage 48.

FIG. 5 illustrates an example fine positioner 42 in use with conduit 46and accumulator stage 48. Conduit 46 is a heatable tubing having a firstend operably connected to or integrally formed with outlet end 80 ofliquefier 68, and a second end operably connected to or integrallyformed with accumulator stage 48. This allows the pressurized moltenmaterial to flow through conduit 46 between stages 44 and 48. In someembodiments, conduit 46 is a tubular conduit (e.g., hollow cylindrical,elliptical, rectangular, etc. . . . ) that is fabricated from athermally and electrically conductive material (e.g., stainless steel).Conduit 46 is also preferably long and thin enough such that accumulatorstage 48 can move relative to liquefier stage 44, at least over smalldistances, without excessive biasing resistance.

Suitable lengths for conduit 46 may vary depending on the particularmounted locations of stages 44 and 48. Examples of suitable lengths forconduit 46 between stages 44 and 48 range from about 51 millimeters(about 2 inches) to about 1 meter (about 40 inches), and in somepreferred embodiments range from about 150 millimeters (about 6 inches)to about 380 millimeters (about 15 inches). In embodiments in whichconduit 46 is cylindrical, examples of suitable outer diameters forconduit 178 range from about 0.635 millimeters (about 0.025 inches) toabout 6.4 millimeters (about 0.25 inches), and in some preferredembodiments range from about 1.37 millimeters (about 0.054 inches) toabout 3.0 millimeters (about 0.12 inches). Similarly, examples ofsuitable hollow inner diameters for conduit 46 range from about 0.58millimeters (about 0.023 inches) to about 6.6 millimeters (about 0.26inches), and in some preferred embodiments range from about 1.3millimeters (about 0.05 inches) to about 3.2 millimeters (about 0.125inches). In embodiments in which conduit 46 is not cylindrical, suitableouter and hollow inner cross-sectional areas include those correspondingto the above discussed outer and hollow inner diameters.

Conduit 46 is preferably heated and/or thermally insulated to preventthe molten material from solidifying during printing operations. Forinstance, conduit 46 may include one or more thermally and/orelectrically insulating casings that enshroud a thermally andelectrically conductive hollow tube core. In the above-discussedembodiment in which conduit 46 is thermally and electrically conductive,a electrical current may be applied to conduit 46 (e.g., via line 36) togenerate resistive heating along conduit 46. Controller assembly 34 mayalso measure and monitor the temperature of conduit 46 in real time fromthe resistance to the applied electrical current (e.g., via line 36).This provides a unique low-mass solution for keeping the molten materialheated as it is pushed through conduit 46 to accumulator stage 48. Inalternative embodiments, conduit 46 may be fabricated from ahigh-temperature polymeric material and encased in a heating sleeve orcoil.

For fine positioner 42, miniactuator 56 is an example robotic mechanismthat includes a pair of rotary voice coil actuators 84 mounted with a90-degree separation arrangement, where each voice coil actuator 84 isconnected to a set of linkage arms 86 that collectively support and moveeffector 58 (and accumulator stage 48) in the x-y plane (and optionallyalong the z-axis). This arrangement of linkage arms 86 effectivelymaintains the same center-of-mass for effector 58 (and accumulator stage48) to pivot around. Additionally, as discussed above, coarse positioner40 may also include other components, such as torque compensator 59, forassisting the operation of miniactuator 56. Based on the torque andangular stroke achievable with each voice coil actuator 84 and thedimensions of linkage arms 86, microactuator 56 is capable of pushing asmall payload with a motion range up to about one-square inch foreffector 58 and accumulator stage 48.

For instance, if each voice coil actuator 84 is capable of generating apeak torque of about 120 ounce-force inches to rotate or pivot linkagearms 86 around their common center, and if the radius of each arm isabout 1.6 inches, the static force on the face each linkage arm 86adjacent to effector 58 is about 4.7 pounds-force. In this case,microactuator 56 is capable of pushing a payload of about 2.2pounds-force. In order to achieve accelerations and decelerations ofabout 50 gees, this results in a payload limit of about 20 grams. Asbriefly discussed above, this requires effector 58 and accumulator stage48 to be low mass.

As mentioned above, in embodiments in which liquefier assembly 20 is asingle-stage liquefier assembly, downstream accumulator stage 48 may bereplaced with an extrusion nozzle. In this case, conduit 46 may extendinto effector 58 and terminate at an extrusion nozzle (e.g.,corresponding to nozzle 90, discussed below). Controller assembly 34 mayaccordingly operate the single-stage liquefier assembly 20 with a drivecontrol determined by liquefier stage 44.

Fine positioner 42 having microactuator 56 is an example of a suitablefine positioner for use with print assembly 20. However, print assembly20 may alternatively incorporate a variety of fine positioners, such asone or more other microactuators, flexure-based piezoelectric stacks,hexapods, Stuart platforms, voice-coil mechanisms, hydraulic-basedactuators, and the like. In fact, in some embodiments, fine positioner42 may move effector 58 and accumulator stage 48 (or an extrusionnozzle) with multiple degrees of movement, such as in an x-y-z range,polar-coordinate movements, rotational movements in the x-y plane, andthe like.

FIGS. 6-8 illustrate an examplary design for accumulator stage 48, whichincludes accumulator 88, nozzle 90, spacers 92, actuator mechanism 94,spacers 96, and heat sink 98. Accumulator 88 is a transverselycompressible and expandable liquefier, which includes opposing faces 88a and opposing lateral ends 88 b, where faces 88 a are the largerdimensions of accumulator 88 (corresponding to the width of accumulator88) and lateral ends 88 b are the smaller dimensions of accumulator 88(corresponding to the thickness of accumulator 88). As with liquefier68, accumulator 88 is also preferably fabricated from one or more rigid,thermally-conductive materials, such as stainless steel, and preferablyhas a ribbon-liquefier geometry (i.e., a hollow liquefier having asubstantially rectangular, arcuate, and/or an elliptical inner-channelcross-section along its longitudinal length).

Accumulator 88 also has an inlet end 100 and an outlet end 102 (shown inFIG. 7), which are preferably offset from each other along longitudinalaxis 104. Inlet end 100 is secured to or integrally formed with conduit46 to receive the molten material from conduit 46. Outlet end 102 is thedownstream portion of accumulator 88 and terminates in nozzle 90.Accumulator 88 may have a length along longitudinal axis 104 rangingfrom about 5 millimeters (about 0.2 inches) to about 25 millimeters(about 1 inch), more preferably from about 8 millimeters (about 0.3inches) to about 18 millimeters (about 0.7 inches). Accumulator stage 48itself may also have these range of lengths.

Suitable hollow, inner-channel thicknesses between faces 88 a range fromabout 0.25 millimeters (about 10 mils) to about 2.5 millimeters (about100 mils), and in some embodiments from about 0.76 millimeters (about 30mils) to about 1.3 millimeters (about 50 mils). Suitable hollow,inner-channel widths between lateral ends 88 b (perpendicular to theinner-channel widths) range from about 2.5 millimeters (about 100 mils)to about 10.2 millimeters (about 400 mils), in some embodiments fromabout 5.1 millimeters (about 200 mils) to about 7.6 millimeters (about300 mils), and in some further embodiments from about 5.7 millimeters(about 225 mils) to about 7.0 millimeters (about 275 mils). Suitablewall thicknesses for accumulator 88 range from about 130 micrometers(about 5 mils) to about 500 micrometers (about 20 mils). Theabove-discussed widths and thicknesses for accumulator 88 are based onthe maximum extents of the widths and thicknesses.

Furthermore, accumulator 88 preferably has wall thicknesses, at least atfaces 88 a, such that when fabricated from one or more polycrystallinemetals, the transverse compression and expansion on faces 88 apreferably generate less than about 0.3% strain. In embodiments in whichaccumulator 88 is fabricated from one or more amorphous metals and/orpolymers, the transverse compression and expansion on faces 88 apreferably generate less than about 3% strain.

Nozzle 90 is a small-diameter nozzle at outlet end 102 of liquefier 88,and is configured to extrude the molten material at a desired roadwidth. Preferred inner tip diameters for nozzle 90 include diameters upto about 760 micrometers (about 0.030 inches), and more preferably rangefrom about 125 micrometers (about 0.005 inches) to about 510 micrometers(about 0.020 inches). In some embodiments, nozzle 90 may include one ormore recessed grooves between annular rings to produce roads havingdifferent road widths, as discussed in Swanson et al., U.S. PublicationNo. 2014/0048969. In other embodiments, nozzle 90 may have larger innertip diameters, such as for large extrudate embodiments.

Nozzle 90 may also have an axial channel with any suitablelength-to-diameter ratio. For example, in some embodiments, nozzle 90may have an axial channel with a length-to-diameter ratio to generatehigh flow resistance, such as a ratio of about 2:1 to about 5:1. Inother embodiments, nozzle 90 may have an axial channel with alength-to-diameter ratio to generate lower flow resistance, such as aratio less than about 1:1. Accordingly, suitable length-to-diameterratios for the axial channel of nozzle 90 may range from about 1:2 toabout 5:1, where in some low-flow resistance embodiments, ratios rangingfrom about 1:2 to about 1:1 may be preferred.

As can be appreciated, when printing 3D part 12 or support structure 14,the extrudate flow from nozzle 90 is rarely held at a constant,steady-state rate. Instead, the extrudate flow rate is typically beingchanged repeatedly to accommodate a variety of different tool pathconditions, such as road start accelerations, road stop decelerations,cornering decelerations and accelerations, road width variations, andthe like.

These flow rate changes are traditionally controlled by adjusting thefeed rate of filament 60 into a liquefier (e.g., liquefier 68 with drivemechanism 62), based on commands from controller assembly 34. Thiscorrespondingly adjusts the pressure generated by the viscosity-pumpaction on the molten material. However, when controller assembly 34commands drive mechanism 62 to change the feed rate of filament 60 intoliquefier 68 (to change the extrudate flow rate from nozzle 90 ofaccumulator stage 48), there is a time response delay between the signalcommand and when the extrusion rate from nozzle 90 actually changes.This is due to response limitations in the motor of drive mechanism 62,the viscosity-pump action in liquefier 68, and the distance betweenstages 44 and 48.

Liquefier assembly 20 may supplement this slower-responding,viscosity-pump action with compressions and expansions of accumulator88. It has been found that liquefiers with particular cross-sectionalgeometries, such as ribbon liquefiers (e.g., accumulator 88), aresusceptible to transversely-applied pressures, and can compress inwardlyand expand outwardly at faces 88 a. For instance, it has been found thataccumulator 88 (and liquefier 68) can expand or balloon transverselyoutward at faces 88 a due to internal pressures that are generatedduring printing operations. These internal pressures are typicallygenerated by the viscosity-pump action of the fed filament 60, and thethermal expansion of the filament material upon melting.

Controller assembly 34 can utilize the compressibility of accumulator 88in a unique manner to generate fast surges of the extrudate from nozzle90 when compressing accumulator 88, and rapid draw backs of theextrudate flow upward from nozzle 90 when accumulator 88 is allowed toexpand. These fast-responding operations can supplement theslower-responding flow rate changes from the viscosity-pump action toimprove extrudate flow accuracies during non-steady-state conditions.

In particular, controller assembly 34 can command actuator mechanism 94to compress and release accumulator 88. In the embodiment shown in FIGS.6-8, actuator mechanism 94 includes two (or more) opposing piezoelectricactuators 106, which are example actuators for quickly generatingtransverse compressions on accumulator 88. As shown, each piezoelectricactuator 106 has a piezoelectric-stack configuration that is securedbetween spacers 92 and 96, and is configured to extend and contractbased on the application of electrical power, such as from line 36.Controller assembly 34 preferably sets a baseline contraction settingfor each piezoelectric actuator 106 at an intermediate state ormid-position between full expansion and full contraction. This allowseach piezoelectric actuator 106 to both contract and extend as needed.Actuator mechanism 94 also preferably includes one or more displacementsensors (e.g., capacitive sensors, not shown) that monitor and/orcorrect displacement errors in piezoelectric actuators 106, which may bedue to hysteresis, thermal effects, and the like. As such, the baselinecontraction settings for piezoelectric actuators 106 may optionally beupdated to account for these displacement errors.

Due to the close proximity of piezoelectric actuators 106 to accumulator88, spacers 92 and 96 preferably thermally isolate piezoelectricactuators 106 from accumulator 88 to protect piezoelectric actuators 106from exposure to excessive heat. In particular, spacers 92 and 96 arepreferably in contact with heat sink 98 to draw heat away fromaccumulator stage 48. Heat sink 98 may have any suitable design, and mayfunction by active and/or passive cooling. For instance, heat sink 98may include multiple fins to dissipate heat from accumulator stage 48,and system 10 may also include one or more cooling fans to generate anair flow around heat sink 98 to increase the heat removal. The heatdissipation from heat sink 98 can also provide a more rapid cool down ofaccumulator 88 when accumulator stage 48 is shut down or placed in astand-by state.

Accumulator stage 48 may also optionally include one or more heaterassemblies (not shown) corresponding to heater assemblies 70. However,as shown in FIG. 7, in one embodiment, accumulator 88 may be adownstream end of conduit 46 that is crushed or otherwise shaped into aribbon-liquefier geometry (e.g., rectangular, elliptical, or arcuate).In this case, heater assemblies 70 may be omitted, particularly ifconduit 46 is thermally and electrically conductive, and is heated by anapplied electrical voltage. Nozzle 90 may also be secured to outlet end102 of accumulator 88, as shown.

During the printing operation, controller assembly 34 may commandpiezoelectric actuators 106 in a synchronized manner such thatpiezoelectric actuators 106 both extend to apply compressive pressureson accumulator 88 (for generating a surge of the molten material), orboth contract to release the transversely-applied pressure fromaccumulator 88 (for generating a drawback of the molten material).

Controller assembly 34 may also command the piezoelectric actuators 106in a variety of different manners, such for providing high-precisionmovements of nozzle 90 along the x-axis. In this case, controllerassembly 34 may command one of piezoelectric actuators 106 to extend,and command the other piezoelectric actuator 106 to contract. This movesaccumulator 88 and nozzle 90 relative to effector 58 along the x-axis,which can supplement any fine-coarse positioning of positioners 40 and42.

For example, as shown in FIG. 8, when controller assembly 34 commandspiezoelectric actuators 106 to extend, as depicted by arrows 108, thissqueezes accumulator 88 and spacers 92 between spacers 96 and heat sink98. Because spacers 92 and 96 are relatively incompressible compared toaccumulator 88, the transversely-applied pressure quickly compressesfaces 88 a of accumulator 88 together, as depicted by arrows 110, whichrapidly reduces the internal volume of accumulator 88 relative to itsinitial cross section. Because the molten material in accumulator 88 isalso relatively incompressible (but squishable or flowable), the quickcompression of accumulator 88 results in a surge or rapid jetting of themolten material from nozzle 90.

Piezoelectric actuators 106 are particularly suitable actuator forcompressing and releasing accumulator 88 in this controlled manner dueto its ability to generate high compressive loads at very fastfrequencies. However, this is only achievable because accumulator 88itself can compress in response to the compressive loads. Piezoelectricactuators 106 preferably compress accumulator 88 along its entirelength, or at least a substantial portion of its entire length. Thisallows a large internal volume of accumulator 88 to be compressedrelative to its surface area, which remains substantially unchanged,thereby allowing a relatively large volume of the molten material to berapidly extruded from nozzle 90 in the surge, if desired.

Additionally, when controller assembly 34 commands piezoelectricactuators 106 to contract, this reduces the transverse pressure appliedto accumulator 88, allowing accumulator 88 to expand back outward, suchas back to its original state (e.g., based on the baseline contractionsetting of piezoelectric actuators 106), or to a fully expanded state(e.g., for extrudate draw back).

As can be appreciated, the compressions applied to accumulator 88 byactuator mechanism 94 are transversely-applied pressures that areexternal to accumulator 88, and are applied to the outer surface ofaccumulator 88 (e.g., at faces 88 a). This is in comparison to internalpressures that are generated by the viscosity-pump action of filament 60or by thermal expansions of the filament material upon melting, or anyother pressures that otherwise affect accumulator 88 from the inside orinterior region of accumulator 88.

FIG. 9 illustrates an example architecture for controller assembly 34 inuse with print assembly 18. Controller assembly 34 may include anysuitable computer-based hardware, such as user interface 112, memorycontroller 114, processor 116, storage media 118, input/output (I/O)controller 120, and communication adapter 122. Controller assembly 34may also include a variety of additional components that are containedin conventional computers, servers, media devices, signal processingdevices, and/or printer controllers.

User interface 112 is a user-operated interface (e.g., keyboards, touchpads, touch-screen displays, display monitors, and other eye, voice,movement, or hand-operated controls) configured to operate controllerassembly 34. Memory controller 114 is a circuit assembly that interfacesthe components of controller assembly 34 with one or more volatilerandom access memory (RAM) modules of storage media 118. Processor 116is one or more computer-processing units configured to operatecontroller assembly 34, optionally with memory controller 114, andpreferably with related processing circuitry (e.g., programmable gatearrays, digital and analog components, and the like). For instance,processor 116 may include one or more microprocessor-based and/ormicrocontroller-based units, one or more central processing units,and/or one or more front-end processing units.

Storage media 118 is one or more internal and/or external data storagedevices or computer storage media for controller assembly 34, such asvolatile RAM modules, read-only memory modules, optical media, magneticmedia (e.g., hard disc drives), solid-state media (e.g., FLASH memoryand solid-state drives), analog media, and the like. Storage media 118may retain an executable copy of processing program 124, and may retainone or more digital models to be printed with system 10, such as digitalmodel 126. Controller assembly 34 may receive digital model 126 overcommunication line 38, where digital model 126 may have any suitablefile format, such as an STL file format, an AMF file format, and thelike.

Processing program 124 is one or more pre-processing and/orpost-processing programs for optionally orienting digital model 126,slicing the oriented digital model 126 into layers, generating supportstructures, generating tool path instructions for printing each slicedlayer with system 10, and the like. I/O controller 120 is a circuitassembly that interfaces memory controller 114, processor 116, andstorage media 118 with various input and output components of controllerassembly 34, including user interface 112 and communication adapter 122.Communication adapter 122 is one or more wired or wirelesstransmitter/receiver adapters configured to communicate overcommunication lines 36 and 38.

The commands from controller assembly 34 to the components of system 10and print assembly 18, such as drive mechanism 62, heater assemblies 70,and actuator mechanism 94, are performed with one or more of userinterface 112, memory controller 114, processor 116, storage media 118,input/output (I/O) controller 120, communication adapter 122, processingprogram 124, and/or other suitable hardware and softwareimplementations, as is understood by those skilled in the art.

Controller assembly 34 can use the compressible nature of accumulator 88in a variety of manners to change the extrudate flow rates fromliquefier assembly 20. For instance, controller assembly 34 can generatelow and high pass signals in a crossover manner for commanding drivemechanism 62 (time-varying, low pass signals) and actuator mechanism 94(time-varying, high pass signals), and store them on storage media 118as one or more data files 130 and 132.

Controller assembly 34 may also generate low and high pass signals in acrossover manner for commanding coarse positioner 40 and fine positioner42, and store them on storage media 118 as one or more data files 134and 136. This allows controller assembly 34 to use the fasteraccelerations and decelerations of fine positioner 42 to supplement theslower accelerations and decelerations of coarse positioner 40, asmentioned above. Controller assembly 34 may then use these data files130-136 with processing program 126 to generate the tool pathinstructions for printing each sliced layer with system 10.

FIGS. 10-12 illustrates an example application for print assembly 18,where FIG. 10 depicts tool path segment 138 following a classic tortuousraster path arrangement, where tool path segment 138 has parallelstraight pathways 140 and 142 connected by a short, 180-degreeturn-around pathway 144. This tool path arrangement produces two corners146 and 148. During the printing operation, controller assembly 34commands coarse positioner 40 to move nozzle 90 of accumulator stage 48along tool path segment 138, while also commanding liquefier assembly 20to extrude the part or support material to print a road that followstool path segment 138.

FIG. 10 also illustrates x-axis velocity plot 150 and y-axis velocityplot 152, which are respective graphical plots of the x-axis velocityand the y-axis velocity for nozzle 90 as it moves along tool pathsegment 138. For a perspective of scale, the length of turn-aroundpathway 144 can be about 20 mils.

As nozzle 90 is moved along pathway 140 in the direction of arrow 154towards corner 146, positioners 40 and 42 may maintain a fast nozzlevelocity (e.g., about 30 inches/second) due to the linear pathway.However, at a given point along pathway 140 (e.g., point 156),controller assembly 34 commands positioners 40 and 42 to deceleratenozzle 90 from the fast nozzle velocity to a slower nozzle velocity(e.g., about 10 inches/second) before reaching corner 146. This isillustrated by a velocity reduction in y-axis velocity plot 152.Positioners 40 and 42 may then negotiate corner 146, and proceed alongpathway 144 in the direction of arrow 158. While passing around corner146, positioners 40 and 42 can briefly accelerate nozzle 90 along thex-axis as shown by x-axis velocity plot 150.

At about a midpoint 160 of pathway 144, while approaching the secondcorner 148, controller assembly 34 commands positioners 40 and 42 todecelerate nozzle 90 along the x-axis, as also shown by x-axis velocityplot 150. Positioners 40 and 42 may then negotiate corner 148, andproceed along pathway 142 in the direction of arrow 162. Controllerassembly 34 may then command positioners 40 and 42 to accelerate nozzle90 back up to the fast nozzle velocity (e.g., about 30 inches/second)upon reaching a point along pathway 142 (e.g., point 164).

FIG. 11 illustrates y-axis position plot 166, which includes signalcomponent 168 for coarse positioner 40, and signal component 170 forfine positioner 42. As positioners 40 and 42 move nozzle 90 alongpathway 140 toward corner 146, the linear motion can be performedentirely by coarse positioner 40, as illustrated by plot segment 172 ofsignal component 168. Thus, controller assembly 34 may command fineposition 42 to remain in a neutral position, and not move accumulatorstage 48 relative to coarse positioner 40.

When negotiating corner 146, pathway 144, and corner 148, controllerassembly 34 may command coarse positioner 40 to decelerate andaccelerate at rates that are low enough such that its natural gantryresonances are not significantly excited, thereby avoiding inducing x-yposition errors. This results in plot segment 174 of signal component168, which itself does not directly follow the x-y coordinates of toolpath 138 at corner 146, pathway 144, and corner 148. Instead, controllerassembly 34 commands fine positioner 42 to move nozzle 90 along the x-ycoordinates of tool path 138, as illustrated by plot segments 176, 178,and 180 of signal component 170, where fine positioner 42 alsodecelerates and accelerates at rates that do not significantly exciteits natural gantry resonances.

After passing corner 148, controller assembly 34 may command finepositioner 42 to return to its neutral position when coarse positioner40 reaches the desired x-y coordinates of tool path 138 along pathway142, as illustrated by plot segment 182 of signal component 168. Thus,plot 168 depicts a scenario where finer positioner 42 supplements themovements of coarse positioner 40. The difference 184 between themaximum y-positions of coarse positioner 40 and fine positioner 42 ispreferably within the range of motion achievable by fine positioner 42along the y-axis (e.g., within about one inch).

As can be appreciated, head gantries having low fundamental resonancefrequencies require longer durations to decelerate nozzle 90 from point156 to corner 146, and to accelerate nozzle 90 from corner 148 to point164. In effect, lower fundamental resonance frequencies move thelocations of points 156 and 164 further away along pathways 140 and 142from corners 146 and 148 due to the slower decelerations andaccelerations.

While the effects of the slower decelerations and accelerations may notbe readily apparent by the placements of points 156 and 164 in FIG. 10,as shown in FIG. 12, liquefier assembly 20 also preferably reduces theextrudate volumetric flow rate from nozzle 90 when nozzle 90 moves atslower velocities, as illustrated by flow rate plot 186. This ispreferred to maintain accurate deposition volumes.

As can be seen in FIG. 12, as positioners 40 and 42 move nozzle 90 alongpathway 140 in the direction of arrow 154 prior to reaching point 156,liquefier assembly 20 can extrude the part or support material fromnozzle 90 at a high flow rate, as illustrated by plot segment 188.However, upon reaching point 156 and decelerating from the fast nozzlevelocity to the slower nozzle velocity while approaching corner 146,liquefier assembly 20 also reduces the volumetric flow rate from nozzle90 from the high flow rate to a lower flow rate (e.g., about one-thirdof the high flow rate). This is illustrated by plot segment 190, andmaintains the same deposited volume for the extrudate road.

While negotiating corner 146, nozzle 90 is moved at its slowest rate.Accordingly, controller assembly 34 may command liquefier assembly 20 tohold the low volumetric flow rate from nozzle 90, as illustrated by plotsegment 192, to match the slower velocity of nozzle 90 at its passesaround corner 146. Then, after passing corner 146, controller assembly34 may command liquefier assembly 20 to increase the volumetric flowrate from nozzle 90, as illustrated by plot segment 194, to match theincreasing velocity of nozzle 90 along the x-axis.

Upon reaching midpoint 160, the above-discussed pattern is reversed, asillustrated by plot segments 196, 198, 200, and 202. The resultingprofile of plot 186 illustrates the reduced volume of extrudate whennegotiating tool path 138 compared to the volume extruded if nozzle 90traveled along a straight tool path at the high velocity and highextrudate flow rate (illustrated by line 204). For example, if the highextrudate flow rate from nozzle 90 (at plot segments 188 and 202) isabout 10,000 micro-cubic inches/second (mics/s) and the low extrudateflow rate from nozzle 90 (at plot segments 192 and 198) is aboutone-third of this (e.g., about 3,333 mics/s), this produces an extrudatevolume reduction of about 30 mics for this turn-around alone.

In comparison, as shown by plot 206 in FIG. 12 (illustrated with brokenlines), for a single-stage gantry having a low resonance frequencycorresponding to coarse positioner 40, the slower deceleration of thegantry requires liquefier assembly 20 to begin reducing the volumetricflow rate from nozzle 90 from the high flow rate to the lower flow rateat point 156 a. This is illustrated by plot segment 208.

Then, between corners 146 and 148, the low volumetric flow rate fromnozzle 90 is held, as illustrated by plot segment 210, to match theslower velocity of nozzle 90. Then, after passing corner 146, thevolumetric flow rate from nozzle 90 may be increased, as illustrated byplot segment 212, to match the increasing velocity of nozzle 90.However, the slower acceleration of the gantry requires liquefierassembly 20 to increase the volumetric flow rate from nozzle 90 at aslower rate to maintain accurate deposition volumes. As such, asillustrated by plot segment 212, the volumetric flow rate from nozzle 90does not reach the high flow rate to the high flow rate at point 164 a.

The resulting profile of plot 206 illustrates the reduced volume ofextrudate when negotiating tool path 138 compared to the volume extrudedif nozzle 90 traveled along a straight tool path at the high velocityand high extrudate flow rate (illustrated by line 204). Following thesame example discussed above, if the high extrudate flow rate fromnozzle 90 is about 10,000 mics/s and the low extrudate flow rate fromnozzle 90 is about one-third of this (e.g., about 3,333 mics/s), thisproduces an extrudate volume reduction of several hundred mics for thisturn-around alone.

As can be seen by comparing the extrudate volume reductions betweenplots 186 and 206, the use of the coarse-fine positioning withpositioners 40 and 42 can result in a significant increase in overallprinting speeds. This is particularly true if tool path 138 is one ofmany tortuous tool paths required to print 3D part 12 (e.g., hundreds orthousands of tortuous tool paths). This can cumulatively result insignificant increases in overall printing speeds, while maintainingaccurate depositions.

Additionally, the higher-frequency movements of fine positioner 42 canalso be used to clean the tip of nozzle 90. For example, a fast lateralflick with an acceleration of about 50 gees can readily break anyextrudate stringing and oozing that may otherwise occur after completinga tool path deposition. This can optionally preclude the need for aseparate purge operation.

Moreover, high-frequency oscillations of effector 58 and accumulatorstage 48 in directions that are normal to the direction of movement canalso cause nozzle 90 to function as a larger nozzle. For instance, ifcoarse positioner 40 and/or fine positioner 42 are moving accumulatorstage 48 along the x-axis, fine positioner 42 may also oscillateaccumulator stage 48 back-and-forth along the y-axis at a high frequencyto effectively increase the deposition range of nozzle 90 along they-axis (i.e., increase the effective size of nozzle 90).

While discussed above as having a ribbon architecture, liquefier stage44 may alternatively include alternative designs, as illustrated inFIGS. 13-15. For example, as shown in FIG. 13, liquefier stage 44 mayinclude a cylindrical liquefier 68 at least partially encased by heaterassembly 70, and which is in use with cylindrical filament 60.Cylindrical liquefier 68 in this embodiment may have any suitabledimensions for melting the cylindrical filament 60, and for pushing thepressurized molten material to conduit 46, as discussed above.

Examples of suitable lengths for cylindrical liquefier 68 in thisembodiment include at least about 1.5 inches, more preferably from about1.5 inches to about 5 inches, and even more preferably from about 50millimeters (about 2 inches) to 76 millimeters (about 3.0 inches).Examples of suitable hollow inner diameters for cylindrical liquefier 68range from about 1.5 millimeters (about 60 mils) to about 2.5millimeters (about 100 mils), and in some embodiments from about 2millimeters (about 80 mils) to about 2.4 millimeters (about 95 mils). Inother embodiments, the hollow inner diameters range from about 1.5millimeters (60 mils) to about 2 millimeters (about 80 mils). Examplesof suitable wall thickness for cylindrical liquefier 68 range from about0.25 millimeters (about 10 mils) to about 0.76 millimeters (about 30mils), and more preferably from about 0.38 millimeters (about 15 mils)to about 0.5 millimeters (about 20 mils).

As shown in FIG. 14, drive mechanism 62 has a screw-pump design with aninternal impeller (not shown) for feeding and melting a consumablematerial in liquefier stage 44. In this embodiment, the consumablematerial may be provided as any suitable media, such as a filament,powder, pellets, or the like, as discussed above. As mentioned above,examples of suitable screw pumps for driving or feeding filamentsinclude those discussed in Skubic et al., U.S. Pat. No. 7,891,964.Examples of suitable screw pumps for driving or feeding powders and/orpellets include those discussed in Bosveld et al., U.S. Publication No.2013/0333798. In other embodiments, drive mechanism 62 may function as adisplacement pump.

As shown in FIG. 15, multiple liquefier stages 44 and conduits 46 feedinto a single accumulator stage 48. As such, accumulator stage 48 can becombined with one or more liquefier stages 44, allowing larger flowrates of the molten materials to be achieved. This embodiment alsoallows different types of consumable materials to be used with the sameaccumulator stage 48. Preferred numbers of liquefier stages 44 andconduits 46 per accumulator stage 48 range from one to six, morepreferably from one to four, and in some embodiments from one to two.

The multiple-stage embodiments shown in FIGS. 13-15 illustrate how theupstream liquefier stage 42 can receive the consumable material in avariety of media forms, and with a variety of different drive mechanismsfor feeding the consumables and generating pressures on the moltenmaterials. As can also be appreciated from the above discussion, thecoordinated operation of the drive mechanism 62 and thefaster-responding actuator mechanism 94 allow controller assembly 34 toprint roads of the molten part and support materials with accurate andconsistent volumes while moving along a variety of different tool pathtrajectories that have non-steady-state conditions, such as road startsand stops, corners, and other conditions where the extrudate flow ratesmay vary.

In addition, the coordinated operation of positioners 40 and 42 allowsprint assembly 18 to produce 3D parts (e.g., 3D part 12) with good partresolutions and fast printing speeds, even when negotiating tortuoustool paths, such as tool paths with sinusoidal geometries, sharpcorners, sharp 180-degree turns, and the like. Moreover, the combinationof the two or more robotic positioners (e.g., positioners 40 and 42) andthe one or more multiple-stage liquefier assemblies (e.g., liquefierassemblies 20) allows controller assembly 34 to print 3D parts andsupport structures with a combination of a coarse-fine position controland a coarse-fine extrusion control.

As mentioned above, one or more portions of print assembly 18, containerportion 22, and guide tube 24 are sub-components of consumable assembly16, such that the given portions of print assembly 18, container portion22, and guide tube 24 are collectively replaced in an interchangeablemanner, as discussed in Swanson, U.S. Pat. No. 8,403,658. For example,in a first embodiment, coarse positioner 42 can be a universal roboticpositioner. In this case, liquefier assembly 20 (including liquefierstage 44, conduit 46, and accumulator stage 48) and fine positioner 42may be removable and interchangeable components that can be secured to(e.g., with a snap-fit mechanism) effector 54. In some embodiments,liquefier assembly 20 and fine positioner 42 may also be sub-componentsof consumable assembly 16, along with container 22 and guide tube 24.

EXAMPLES

The present disclosure is more particularly described in the followingexamples that are intended as illustrations only, since numerousmodifications and variations within the scope of the present disclosurewill be apparent to those skilled in the art.

A test was performed to determine whether a conduit (e.g., correspondingto conduit 46) is capable of self heating under an applied electricalcurrent. FIG. 16 is an infrared image of the test conduit beingelectrically heated. The conduit was a 14-gauge 304-stainless steeltubing, 12-inches long, with an 84 mil outer diameter, and 10 mil wallthickness. 12-gauge copper wires (3-feet in length) connected theconduit to a 10-ampere power supply, which required about 1.9 Volts ofdrive. The copper wires were brazed to the conduit with Muggy Weld SSF-6silver solder using a propane torch. As shown in FIG. 16, pushing 10amperes through the conduit raised the temperature of the conduit toabout 90° C. in ambient air. This illustrates that the conduits,liquefiers, and accumulators of the present disclosure are capable ofself heating under applied electrical currents.

Although the present disclosure has been described with reference topreferred embodiments, workers skilled in the art will recognize thatchanges may be made in form and detail without departing from the spiritand scope of the disclosure. Applicant hereby incorporates by referenceU.S. Provisional Application Ser. No. 62/056,186 entitled LIQUEFIERASSEMBLIES FOR ADDITIVE MANUFACTURING SYSTEMS, AND METHODS OF USETHEREOF filed on Sep. 26, 2014 in its entirety herein.

The invention claimed is:
 1. A print assembly for use in an additivemanufacturing system to print three-dimensional parts, the printassembly comprising: a coarse gantry; a fine gantry operably mounted tothe coarse gantry such that the coarse gantry is configured to move thefine gantry, and wherein the fine gantry has a higher fundamentalresonance frequency than the coarse gantry; and a liquefier assemblyconfigured to heat an extrudable material to a molten state and extrudethe molten material, wherein at least a portion of the liquefierassembly is operably mounted to the fine gantry; wherein the fine gantryexecutes toolpaths with the portion of the liquefier assembly at leastat 30 gees without significant toolpath errors.
 2. The print assembly ofclaim 1, wherein the fine gantry executes toolpaths with the portion ofthe liquefier assembly at least at 40 gees without significant toolpatherrors.
 3. The print assembly of claim 1, wherein the fine gantryexecutes toolpaths with the portion of the liquefier assembly at leastat 50 gees without significant toolpath errors.
 4. The print assembly ofclaim 1, wherein the portion of the liquefier assembly that is operablymounted to the fine gantry has a mass of less than 50 grams.
 5. Theprint assembly of claim 1, wherein the portion of the liquefier assemblythat is operably mounted to the fine gantry comprises: an accumulator; anozzle at an outlet end of the accumulator; and an actuator mechanismconfigured to controllably apply pressure to transversely compress theaccumulator.
 6. The print assembly of claim 5, wherein the liquefierassembly further comprises: a drive mechanism; a liquefier configured toreceive a consumable material from the drive mechanism; and one or morefirst heater assemblies configured to heat the liquefier for heating thereceived consumable material to a molten state.
 7. The print assembly ofclaim 6, wherein the liquefier assembly further comprises a conduitconfigured to receive the molten consumable material from the liquefier.8. The print assembly of claim 1, wherein the fine gantry comprises oneor more voice coil actuators or one or more piezoelectric actuators. 9.The print assembly of claim 1, wherein the fine gantry moves in a x-yplane.
 10. The print assembly of claim 1, wherein the fine gantry movesin along x, y and z axes.
 11. The print assembly of claim 1, wherein thefine gantry moves in a polar coordinate system.
 12. The print assemblyof claim 1, wherein the fine gantry moves in a x-y plane along withrotational movement.
 13. The print assembly of claim 1, wherein thecoarse gantry is configured to move in a plane.
 14. The print assemblyof claim 1, wherein the coarse gantry is configured to move in five axesof motion.
 15. A method of printing a 3D part with an extrusion-basedadditive manufacturing system, the method comprising: providing a printassembly having a fine gantry carried by a coarse gantry, the finegantry having a higher fundamental resonance relative to the coursegantry and wherein the fine gantry carries at least a portion of aliquefier with an extrusion nozzle, wherein the at least a portion ofthe liquefier assembly that is operably mounted to the fine gantry has amass of less than 50 grams; extruding a molten material through theextrusion nozzle while navigating the coarse gantry along a firstportion of a toolpath; and extruding the molten material through theextrusion nozzle while navigating the fine gantry along a second portionof the toolpath wherein the fine gantry executes the second portion ofthe toolpath with the portion of the liquefier assembly at least at 30gees without significant toolpath errors.
 16. The method of claim 15,wherein the fine gantry executes the second portion of the toolpath atleast at 40 gees without significant toolpath errors.
 17. The method ofclaim 15, wherein the fine executes the second portion of the toolpathat least at 50 gees without significant toolpath errors.
 18. The methodof claim 15, wherein navigating the second portion of the toolpathcomprises moving the fine gantry within one square inch of travel. 19.The method of claim 15, wherein navigating the fine gantry along thesecond portion of the tool path comprises motion in a x-y plane.
 20. Themethod of claim 15, wherein navigating the fine gantry along the secondportion of the tool path comprises motion in along a x, y and z axes.21. The method of claim 15, wherein navigating the fine gantry along thesecond portion of the tool path comprises motion utilizing polarcoordinates.
 22. The method of claim 15, wherein navigating the finegantry along the second portion of the tool path comprises motion in ax-y plane along with rotational movement.
 23. The method of claim 15,wherein the at least the portion of the liquefier comprises anaccumulator in fluid communication with the extrusion nozzle and anactuator, the method comprising compressing or releasing pressure on theaccumulator with the actuator to adjust a flow rate from the nozzle. 24.The method of claim 15, wherein the second portion of the toolpathcomprises sinusoidal geometries, sharp corners and/or sharp 180-degreeturns.
 25. The method of claim 15, wherein the coarse gantry moves in aplane.
 26. The method of claim 15, wherein the coarse gantry moves infive axes of motion.